30-21-00
ALL ú
ú 01 Page 101
ú Dec 20/93
D05250
A
757 FAULT ISOLATION/MAINT MANUAL
ENGINE/WING ANTI-ICE CONTROL PANEL, M10397 (REF)
SWITCH-LIGHT (S1) SWITCH-LIGHT (S2)
ENGINE/WING ANTI-ICE CONTROL PANEL, M10397 (REF)
Engine Inlet Thermal Anti-Ice System - Component Location
Figure 102 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-21-00
ALL ú
ú 01 Page 102
ú Sep 20/97
A
757
FAULT ISOLATION/MAINT MANUAL
ENGINE INLET ANTI-ICE DUCT (REF)
423AL 413AL, RB211-535E4 ENGINE INLET 2 SEE B TAI PRESSURE (POP-OUT) INDICATOR 3 423AL 413AL, SWITCHES PRESSURE ANTI-ICE THERMAL ANTI-ICE VALVE, V10028 SEE C
SEE D
RB211-535E4 ENGINE INLET
B
1 ENGINE INLET THERMAL ANTI-ICE VALVE, V10028 SWITCH, S10137 HIGH PRESSURE ANTI-ICE ENGINE INLET
ENGINE INLET ANTI-ICE LOW PRESSURE SWITCH, S10135
THERMAL ANTI-ICE VALVE, V10028
C
ENGINE INLET ANTI-ICE 1
ENGINES WITHOUT THE VALVE POSITION INDICATOR SWITCH PRESSURE SWITCHES (ONE ELECTRICAL CONNECTOR ON THE VALVE)
2
ENGINES WITH THE VALVE POSITION INDICATOR SWITCH D
(TWO ELECTRICAL CONNECTORS ON THE VALVE)
3 ENGINES WITH RR SB 71-9634
Engine Inlet Thermal Anti-Ice System - Component Location
Figure 102 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-21-00
ALL ú ú 01 Page 103 ú Dec 20/93
A
757 MAINTENANCE MANUAL
ENGINE INLET THERMAL ANTI-ICING - ADJUSTMENT/TEST
_________________________________________________
1. General
A. This procedure contains two tasks. The first task is the system test of the engine inlet thermal anti-icing system. The second task is the scheduled maintenance test procedure for the engine thermal anti-ice system.
TASK 30-21-00-735-001
2. System Test - Engine Inlet Thermal Anti-Ice (TAI) System
________________________________________________________
A. General
(1) The left and right engine inlet TAI system tests are given in this task.
B. Equipment
(1) Volt-ohmmeter - Simpson 260
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：757 AMM 飞机维护手册 防冰和排雨 CHAPTER 30 - ICE AND RAIN PROTECTION(51)
